mirror of
https://github.com/ArduPilot/ardupilot
synced 2025-01-22 00:28:30 -04:00
PX4: added in remaining example mixers
This commit is contained in:
parent
947297f0cd
commit
9b752f5d2a
64
mk/PX4/ROMFS/mixers/FMU_AERT.mix
Normal file
64
mk/PX4/ROMFS/mixers/FMU_AERT.mix
Normal file
@ -0,0 +1,64 @@
|
||||
Aileron/rudder/elevator/throttle mixer for PX4FMU
|
||||
==================================================
|
||||
|
||||
This file defines mixers suitable for controlling a fixed wing aircraft with
|
||||
aileron, rudder, elevator and throttle controls using PX4FMU. The configuration
|
||||
assumes the aileron servo(s) are connected to PX4FMU servo output 0, the
|
||||
elevator to output 1, the rudder to output 2 and the throttle to output 3.
|
||||
|
||||
Inputs to the mixer come from channel group 0 (vehicle attitude), channels 0
|
||||
(roll), 1 (pitch) and 3 (thrust).
|
||||
|
||||
Aileron mixer
|
||||
-------------
|
||||
Two scalers total (output, roll).
|
||||
|
||||
This mixer assumes that the aileron servos are set up correctly mechanically;
|
||||
depending on the actual configuration it may be necessary to reverse the scaling
|
||||
factors (to reverse the servo movement) and adjust the offset, scaling and
|
||||
endpoints to suit.
|
||||
|
||||
As there is only one output, if using two servos adjustments to compensate for
|
||||
differences between the servos must be made mechanically. To obtain the correct
|
||||
motion using a Y cable, the servos can be positioned reversed from one another.
|
||||
|
||||
M: 1
|
||||
O: 10000 10000 0 -10000 10000
|
||||
S: 0 0 10000 10000 0 -10000 10000
|
||||
|
||||
Elevator mixer
|
||||
------------
|
||||
Two scalers total (output, roll).
|
||||
|
||||
This mixer assumes that the elevator servo is set up correctly mechanically;
|
||||
depending on the actual configuration it may be necessary to reverse the scaling
|
||||
factors (to reverse the servo movement) and adjust the offset, scaling and
|
||||
endpoints to suit.
|
||||
|
||||
M: 1
|
||||
O: 10000 10000 0 -10000 10000
|
||||
S: 0 1 -10000 -10000 0 -10000 10000
|
||||
|
||||
Rudder mixer
|
||||
------------
|
||||
Two scalers total (output, yaw).
|
||||
|
||||
This mixer assumes that the rudder servo is set up correctly mechanically;
|
||||
depending on the actual configuration it may be necessary to reverse the scaling
|
||||
factors (to reverse the servo movement) and adjust the offset, scaling and
|
||||
endpoints to suit.
|
||||
|
||||
M: 1
|
||||
O: 10000 10000 0 -10000 10000
|
||||
S: 0 2 10000 10000 0 -10000 10000
|
||||
|
||||
Motor speed mixer
|
||||
-----------------
|
||||
Two scalers total (output, thrust).
|
||||
|
||||
This mixer generates a full-range output (-1 to 1) from an input in the (0 - 1)
|
||||
range. Inputs below zero are treated as zero.
|
||||
|
||||
M: 1
|
||||
O: 10000 10000 0 -10000 10000
|
||||
S: 0 3 0 20000 -10000 -10000 10000
|
60
mk/PX4/ROMFS/mixers/FMU_AET.mix
Normal file
60
mk/PX4/ROMFS/mixers/FMU_AET.mix
Normal file
@ -0,0 +1,60 @@
|
||||
Aileron/elevator/throttle mixer for PX4FMU
|
||||
==================================================
|
||||
|
||||
This file defines mixers suitable for controlling a fixed wing aircraft with
|
||||
aileron, elevator and throttle controls using PX4FMU. The configuration assumes
|
||||
the aileron servo(s) are connected to PX4FMU servo output 0, the elevator to
|
||||
output 1 and the throttle to output 3.
|
||||
|
||||
Inputs to the mixer come from channel group 0 (vehicle attitude), channels 0
|
||||
(roll), 1 (pitch) and 3 (thrust).
|
||||
|
||||
Aileron mixer
|
||||
-------------
|
||||
Two scalers total (output, roll).
|
||||
|
||||
This mixer assumes that the aileron servos are set up correctly mechanically;
|
||||
depending on the actual configuration it may be necessary to reverse the scaling
|
||||
factors (to reverse the servo movement) and adjust the offset, scaling and
|
||||
endpoints to suit.
|
||||
|
||||
As there is only one output, if using two servos adjustments to compensate for
|
||||
differences between the servos must be made mechanically. To obtain the correct
|
||||
motion using a Y cable, the servos can be positioned reversed from one another.
|
||||
|
||||
Alternatively, output 2 could be used as a second aileron servo output with
|
||||
separate mixing.
|
||||
|
||||
M: 1
|
||||
O: 10000 10000 0 -10000 10000
|
||||
S: 0 0 10000 10000 0 -10000 10000
|
||||
|
||||
Elevator mixer
|
||||
------------
|
||||
Two scalers total (output, roll).
|
||||
|
||||
This mixer assumes that the elevator servo is set up correctly mechanically;
|
||||
depending on the actual configuration it may be necessary to reverse the scaling
|
||||
factors (to reverse the servo movement) and adjust the offset, scaling and
|
||||
endpoints to suit.
|
||||
|
||||
M: 1
|
||||
O: 10000 10000 0 -10000 10000
|
||||
S: 0 1 -10000 -10000 0 -10000 10000
|
||||
|
||||
Output 2
|
||||
--------
|
||||
This mixer is empty.
|
||||
|
||||
Z:
|
||||
|
||||
Motor speed mixer
|
||||
-----------------
|
||||
Two scalers total (output, thrust).
|
||||
|
||||
This mixer generates a full-range output (-1 to 1) from an input in the (0 - 1)
|
||||
range. Inputs below zero are treated as zero.
|
||||
|
||||
M: 1
|
||||
O: 10000 10000 0 -10000 10000
|
||||
S: 0 3 0 20000 -10000 -10000 10000
|
52
mk/PX4/ROMFS/mixers/FMU_Q.mix
Normal file
52
mk/PX4/ROMFS/mixers/FMU_Q.mix
Normal file
@ -0,0 +1,52 @@
|
||||
Delta-wing mixer for PX4FMU
|
||||
===========================
|
||||
|
||||
Designed for Bormatec Camflyer Q
|
||||
|
||||
This file defines mixers suitable for controlling a delta wing aircraft using
|
||||
PX4FMU. The configuration assumes the elevon servos are connected to PX4FMU
|
||||
servo outputs 0 and 1 and the motor speed control to output 3. Output 2 is
|
||||
assumed to be unused.
|
||||
|
||||
Inputs to the mixer come from channel group 0 (vehicle attitude), channels 0
|
||||
(roll), 1 (pitch) and 3 (thrust).
|
||||
|
||||
See the README for more information on the scaler format.
|
||||
|
||||
Elevon mixers
|
||||
-------------
|
||||
Three scalers total (output, roll, pitch).
|
||||
|
||||
On the assumption that the two elevon servos are physically reversed, the pitch
|
||||
input is inverted between the two servos.
|
||||
|
||||
The scaling factor for roll inputs is adjusted to implement differential travel
|
||||
for the elevons.
|
||||
|
||||
M: 2
|
||||
O: 10000 10000 0 -10000 10000
|
||||
S: 0 0 -5000 -8000 0 -10000 10000
|
||||
S: 0 1 8000 8000 0 -10000 10000
|
||||
|
||||
M: 2
|
||||
O: 10000 10000 0 -10000 10000
|
||||
S: 0 0 -8000 -5000 0 -10000 10000
|
||||
S: 0 1 -8000 -8000 0 -10000 10000
|
||||
|
||||
Output 2
|
||||
--------
|
||||
This mixer is empty.
|
||||
|
||||
Z:
|
||||
|
||||
Motor speed mixer
|
||||
-----------------
|
||||
Two scalers total (output, thrust).
|
||||
|
||||
This mixer generates a full-range output (-1 to 1) from an input in the (0 - 1)
|
||||
range. Inputs below zero are treated as zero.
|
||||
|
||||
M: 1
|
||||
O: 10000 10000 0 -10000 10000
|
||||
S: 0 3 0 20000 -10000 -10000 10000
|
||||
|
53
mk/PX4/ROMFS/mixers/FMU_RET.mix
Normal file
53
mk/PX4/ROMFS/mixers/FMU_RET.mix
Normal file
@ -0,0 +1,53 @@
|
||||
Rudder/elevator/throttle mixer for PX4FMU
|
||||
=========================================
|
||||
|
||||
This file defines mixers suitable for controlling a fixed wing aircraft with
|
||||
rudder, elevator and throttle controls using PX4FMU. The configuration assumes
|
||||
the rudder servo is connected to PX4FMU servo output 0, the elevator to output 1
|
||||
and the throttle to output 3.
|
||||
|
||||
Inputs to the mixer come from channel group 0 (vehicle attitude), channels 0
|
||||
(roll), 1 (pitch) and 3 (thrust).
|
||||
|
||||
Rudder mixer
|
||||
------------
|
||||
Two scalers total (output, roll).
|
||||
|
||||
This mixer assumes that the rudder servo is set up correctly mechanically;
|
||||
depending on the actual configuration it may be necessary to reverse the scaling
|
||||
factors (to reverse the servo movement) and adjust the offset, scaling and
|
||||
endpoints to suit.
|
||||
|
||||
M: 1
|
||||
O: 10000 10000 0 -10000 10000
|
||||
S: 0 0 10000 10000 0 -10000 10000
|
||||
|
||||
Elevator mixer
|
||||
------------
|
||||
Two scalers total (output, roll).
|
||||
|
||||
This mixer assumes that the elevator servo is set up correctly mechanically;
|
||||
depending on the actual configuration it may be necessary to reverse the scaling
|
||||
factors (to reverse the servo movement) and adjust the offset, scaling and
|
||||
endpoints to suit.
|
||||
|
||||
M: 1
|
||||
O: 10000 10000 0 -10000 10000
|
||||
S: 0 1 -10000 -10000 0 -10000 10000
|
||||
|
||||
Output 2
|
||||
--------
|
||||
This mixer is empty.
|
||||
|
||||
Z:
|
||||
|
||||
Motor speed mixer
|
||||
-----------------
|
||||
Two scalers total (output, thrust).
|
||||
|
||||
This mixer generates a full-range output (-1 to 1) from an input in the (0 - 1)
|
||||
range. Inputs below zero are treated as zero.
|
||||
|
||||
M: 1
|
||||
O: 10000 10000 0 -10000 10000
|
||||
S: 0 3 0 20000 -10000 -10000 10000
|
50
mk/PX4/ROMFS/mixers/FMU_X5.mix
Normal file
50
mk/PX4/ROMFS/mixers/FMU_X5.mix
Normal file
@ -0,0 +1,50 @@
|
||||
Delta-wing mixer for PX4FMU
|
||||
===========================
|
||||
|
||||
This file defines mixers suitable for controlling a delta wing aircraft using
|
||||
PX4FMU. The configuration assumes the elevon servos are connected to PX4FMU
|
||||
servo outputs 0 and 1 and the motor speed control to output 3. Output 2 is
|
||||
assumed to be unused.
|
||||
|
||||
Inputs to the mixer come from channel group 0 (vehicle attitude), channels 0
|
||||
(roll), 1 (pitch) and 3 (thrust).
|
||||
|
||||
See the README for more information on the scaler format.
|
||||
|
||||
Elevon mixers
|
||||
-------------
|
||||
Three scalers total (output, roll, pitch).
|
||||
|
||||
On the assumption that the two elevon servos are physically reversed, the pitch
|
||||
input is inverted between the two servos.
|
||||
|
||||
The scaling factor for roll inputs is adjusted to implement differential travel
|
||||
for the elevons.
|
||||
|
||||
M: 2
|
||||
O: 10000 10000 0 -10000 10000
|
||||
S: 0 0 -3000 -5000 0 -10000 10000
|
||||
S: 0 1 -5000 -5000 0 -10000 10000
|
||||
|
||||
M: 2
|
||||
O: 10000 10000 0 -10000 10000
|
||||
S: 0 0 -5000 -3000 0 -10000 10000
|
||||
S: 0 1 5000 5000 0 -10000 10000
|
||||
|
||||
Output 2
|
||||
--------
|
||||
This mixer is empty.
|
||||
|
||||
Z:
|
||||
|
||||
Motor speed mixer
|
||||
-----------------
|
||||
Two scalers total (output, thrust).
|
||||
|
||||
This mixer generates a full-range output (-1 to 1) from an input in the (0 - 1)
|
||||
range. Inputs below zero are treated as zero.
|
||||
|
||||
M: 1
|
||||
O: 10000 10000 0 -10000 10000
|
||||
S: 0 3 0 20000 -10000 -10000 10000
|
||||
|
50
mk/PX4/ROMFS/mixers/FMU_delta.mix
Normal file
50
mk/PX4/ROMFS/mixers/FMU_delta.mix
Normal file
@ -0,0 +1,50 @@
|
||||
Delta-wing mixer for PX4FMU
|
||||
===========================
|
||||
|
||||
This file defines mixers suitable for controlling a delta wing aircraft using
|
||||
PX4FMU. The configuration assumes the elevon servos are connected to PX4FMU
|
||||
servo outputs 0 and 1 and the motor speed control to output 3. Output 2 is
|
||||
assumed to be unused.
|
||||
|
||||
Inputs to the mixer come from channel group 0 (vehicle attitude), channels 0
|
||||
(roll), 1 (pitch) and 3 (thrust).
|
||||
|
||||
See the README for more information on the scaler format.
|
||||
|
||||
Elevon mixers
|
||||
-------------
|
||||
Three scalers total (output, roll, pitch).
|
||||
|
||||
On the assumption that the two elevon servos are physically reversed, the pitch
|
||||
input is inverted between the two servos.
|
||||
|
||||
The scaling factor for roll inputs is adjusted to implement differential travel
|
||||
for the elevons.
|
||||
|
||||
M: 2
|
||||
O: 10000 10000 0 -10000 10000
|
||||
S: 0 0 3000 5000 0 -10000 10000
|
||||
S: 0 1 5000 5000 0 -10000 10000
|
||||
|
||||
M: 2
|
||||
O: 10000 10000 0 -10000 10000
|
||||
S: 0 0 5000 3000 0 -10000 10000
|
||||
S: 0 1 -5000 -5000 0 -10000 10000
|
||||
|
||||
Output 2
|
||||
--------
|
||||
This mixer is empty.
|
||||
|
||||
Z:
|
||||
|
||||
Motor speed mixer
|
||||
-----------------
|
||||
Two scalers total (output, thrust).
|
||||
|
||||
This mixer generates a full-range output (-1 to 1) from an input in the (0 - 1)
|
||||
range. Inputs below zero are treated as zero.
|
||||
|
||||
M: 1
|
||||
O: 10000 10000 0 -10000 10000
|
||||
S: 0 3 0 20000 -10000 -10000 10000
|
||||
|
7
mk/PX4/ROMFS/mixers/FMU_hex_+.mix
Normal file
7
mk/PX4/ROMFS/mixers/FMU_hex_+.mix
Normal file
@ -0,0 +1,7 @@
|
||||
Multirotor mixer for PX4FMU
|
||||
===========================
|
||||
|
||||
This file defines a single mixer for a hexacopter in the + configuration. All controls
|
||||
are mixed 100%.
|
||||
|
||||
R: 6+ 10000 10000 10000 0
|
7
mk/PX4/ROMFS/mixers/FMU_hex_x.mix
Normal file
7
mk/PX4/ROMFS/mixers/FMU_hex_x.mix
Normal file
@ -0,0 +1,7 @@
|
||||
Multirotor mixer for PX4FMU
|
||||
===========================
|
||||
|
||||
This file defines a single mixer for a hexacopter in the X configuration. All controls
|
||||
are mixed 100%.
|
||||
|
||||
R: 6x 10000 10000 10000 0
|
7
mk/PX4/ROMFS/mixers/FMU_octo_+.mix
Normal file
7
mk/PX4/ROMFS/mixers/FMU_octo_+.mix
Normal file
@ -0,0 +1,7 @@
|
||||
Multirotor mixer for PX4FMU
|
||||
===========================
|
||||
|
||||
This file defines a single mixer for a octocopter in the + configuration. All controls
|
||||
are mixed 100%.
|
||||
|
||||
R: 8+ 10000 10000 10000 0
|
7
mk/PX4/ROMFS/mixers/FMU_octo_x.mix
Normal file
7
mk/PX4/ROMFS/mixers/FMU_octo_x.mix
Normal file
@ -0,0 +1,7 @@
|
||||
Multirotor mixer for PX4FMU
|
||||
===========================
|
||||
|
||||
This file defines a single mixer for a octocopter in the X configuration. All controls
|
||||
are mixed 100%.
|
||||
|
||||
R: 8x 10000 10000 10000 0
|
7
mk/PX4/ROMFS/mixers/FMU_quad_+.mix
Normal file
7
mk/PX4/ROMFS/mixers/FMU_quad_+.mix
Normal file
@ -0,0 +1,7 @@
|
||||
Multirotor mixer for PX4FMU
|
||||
===========================
|
||||
|
||||
This file defines a single mixer for a quadrotor in the + configuration. All controls
|
||||
are mixed 100%.
|
||||
|
||||
R: 4+ 10000 10000 10000 0
|
7
mk/PX4/ROMFS/mixers/FMU_quad_v.mix
Normal file
7
mk/PX4/ROMFS/mixers/FMU_quad_v.mix
Normal file
@ -0,0 +1,7 @@
|
||||
Multirotor mixer for PX4FMU
|
||||
===========================
|
||||
|
||||
This file defines a single mixer for a quadrotor in the V configuration. All controls
|
||||
are mixed 100%.
|
||||
|
||||
R: 4v 10000 10000 10000 0
|
7
mk/PX4/ROMFS/mixers/FMU_quad_x.mix
Normal file
7
mk/PX4/ROMFS/mixers/FMU_quad_x.mix
Normal file
@ -0,0 +1,7 @@
|
||||
Multirotor mixer for PX4FMU
|
||||
===========================
|
||||
|
||||
This file defines a single mixer for a quadrotor in the X configuration. All controls
|
||||
are mixed 100%.
|
||||
|
||||
R: 4x 10000 10000 10000 0
|
Loading…
Reference in New Issue
Block a user